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Two candidate single-stage rockets are proposed for a specified mission with a required V = 10,000 m/s and a payload mass of 10,000 kg. The

Two candidate single-stage rockets are proposed for a specified mission with a required V = 10,000 m/s and a payload mass of 10,000 kg. The first rocket (rocket A) is a chemical rocket. The second rocket (rocket B) is an electric rocket

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